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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
|
tailwheel configuration
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gptkbp:aircraft_operated
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utility aircraft
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gptkbp:cockpit
|
enclosed cockpit
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gptkbp:control_surfaces
|
elevator, ailerons, rudder
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gptkbp:country_of_origin
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gptkb:United_States
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gptkbp:crew
|
gptkb:1
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gptkbp:cruise_speed
|
120 mph
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gptkbp:design
|
W. M. Stinson
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gptkbp:engine_power
|
165 hp
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gptkbp:engine_type
|
gptkb:radial_engine
|
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gptkbp:first_flight
|
1946
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gptkbp:fuel_capacity
|
40 US gallons
|
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gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
8 ft 0 in
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gptkbp:historical_significance
|
popular post-war aircraft
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Stinson Voyager
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gptkbp:influenced_by
|
gptkb:Stinson_Reliant
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gptkbp:landing_distance
|
60 mph
1,000 ft
|
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gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
25 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Stinson_Aircraft_Company
|
|
gptkbp:market_segment
|
private pilots
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gptkbp:marketed_as
|
gptkb:Stinson_108
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|
gptkbp:max_takeoff_weight
|
2,800 lb
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gptkbp:notable_features
|
high-wing design
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|
gptkbp:number_built
|
approximately 1,000
|
|
gptkbp:offers_certificate
|
gptkb:Type_Certificate_A-754
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|
gptkbp:operational_history
|
used in various roles including training and personal use
|
|
gptkbp:passenger_capacity
|
gptkb:3
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|
gptkbp:production_location
|
gptkb:Nashville,_Tennessee
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|
gptkbp:production_years
|
1946-1949
|
|
gptkbp:propeller
|
two-blade propeller
|
|
gptkbp:range
|
600 miles
|
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gptkbp:retirement
|
1970s
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gptkbp:role
|
general aviation
|
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gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:stall_speed
|
50 mph
|
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gptkbp:successor
|
gptkb:Stinson_108-3
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gptkbp:tail_type
|
conventional tail
|
|
gptkbp:takeoff_distance
|
1,200 ft
|
|
gptkbp:transportation
|
20 mph
|
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gptkbp:type
|
gptkb:light_aircraft
|
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gptkbp:variant
|
gptkb:Stinson_108-1
gptkb:Stinson_108-2
gptkb:Stinson_108-3
gptkb:Stinson_108-5
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|
gptkbp:wing_area
|
200 sq ft
|
|
gptkbp:wing_configuration
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gptkb:metal
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|
gptkbp:wingspan
|
36 ft 0 in
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gptkbp:bfsParent
|
gptkb:Stinson_Aircraft_Company
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gptkbp:bfsLayer
|
7
|